EP 3172130 A1 20170531 - AIRCRAFT WITH WING-BORNE FLIGHT MODE AND HOVER FLIGHT MODE
Title (en)
AIRCRAFT WITH WING-BORNE FLIGHT MODE AND HOVER FLIGHT MODE
Title (de)
FLUGZEUG MIT FLÜGELGETRAGENEM FLUGMODUS UND SCHWEBEFLUGMODUS
Title (fr)
AÉRONEF AVEC UN MODE DE VOL PORTÉ PAR L'AILE ET UN MODE DE VOL STATIONNAIRE
Publication
Application
Priority
- NL 2013252 A 20140724
- NL 2015050531 W 20150721
Abstract (en)
[origin: WO2016013933A1] An aircraft, in particular an unmanned aerial vehicle with wing-borne flight mode and hover flight mode, comprises a wing structure (4) having a left (6), middle (7), and right wing section (8). A support structure extends from the wing structure (4), and has an upper and lower support section. Each one of the left and right wing section (6, 8), and upper and lower support section (18, 20) has a thrust unit (10, 12, 22, 24). Left and right wingtip sections are rotatable relative to a left and right wing base section, respectively, around an axis extending substantially in a lengthwise direction of the wing structure. The thrust units (10,1 2) of the left and right wing sections(6, 8) are provided at the respective wingtip sections, in particular at the extremities thereof.
IPC 8 full level
B64C 39/02 (2006.01)
CPC (source: EP US)
B64C 29/02 (2013.01 - US); B64U 10/25 (2023.01 - EP US); B64U 30/10 (2023.01 - EP US); B64U 50/13 (2023.01 - EP US); B64U 50/19 (2023.01 - EP US); B64U 70/80 (2023.01 - EP US)
Citation (search report)
See references of WO 2016013933A1
Designated contracting state (EPC)
AL AT BE BG CH CY CZ DE DK EE ES FI FR GB GR HR HU IE IS IT LI LT LU LV MC MK MT NL NO PL PT RO RS SE SI SK SM TR
Designated extension state (EPC)
BA ME
DOCDB simple family (publication)
WO 2016013933 A1 20160128; EP 3172130 A1 20170531; EP 3172130 B1 20181003; ES 2703353 T3 20190308; NL 2013252 B1 20160909; PL 3172130 T3 20190531; US 10913531 B2 20210209; US 2017217585 A1 20170803
DOCDB simple family (application)
NL 2015050531 W 20150721; EP 15747241 A 20150721; ES 15747241 T 20150721; NL 2013252 A 20140724; PL 15747241 T 20150721; US 201515328611 A 20150721